Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
By: Donald R. Riley and Gautam H. Shah, Richard E Kuhn.
Contributors: Shah, Gautam H.; Kuhn, Richard E.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Series: NASA technical memorandum -- 4147.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; For sale by the National Technical Information Service]
Published: 1989
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 36
Subjects: Short take-off and landing aircraft.; Vertically rising aircraft.; Airplanes -- Control systems -- Testing.; Attitude control.; Fighter aircraft.; Hovering.; Jet flow.; Short takeoff aircraft.; Wind tunnel tests.
Other titles: Low speed wind tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept.
Notes: Shipping list no.: 90-0669-M.

"Performing organization report no.: L-16616"--Technical rept. documentation p.

Includes bibliographical references (p. 11).

Also available via Internet from the NASA Technical Report Server web site. Address as of 7/28/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900002435%5F1990002435.pdf; current access available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990]. 1 microfiche : negative.

505-61-71-07.